View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 55631U 26145.35126991 +.00000000 +00000-0 +12135-4 0 00003
2 55631 70.0005 11.0734 0002570 269.6389 90.4476 14.98330399 06
| Epoch (UTC): | 25 May 2026 08:25:49 |
| Eccentricity: | 0.0002570 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 11.0734° |
| argument of perigee: | 269.6389° |
| revolutions per day: | 14.98330399 |
| mean anomaly at epoch: | 90.4476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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